IP Library Granted Patent US 10,796,586
Granted Patent B2
US 10,796,586 · App. 14/966,988 · Granted Oct 6, 2020

Weather avoidance tool system

Inventor: William Henry Watts (Seneca, SC)
Assignee: Delta Air Lines, Inc.
G08G5/0034G01C21/3407G08G5/0021G08G5/0091G01W2001/003
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Quick Facts
Patent No.
US 10,796,586
App. No.
14/966,988
Granted
Oct 6, 2020
Kind
B2
Abstract

A method of providing a simplified practice for dealing with aviation turbulence and other weather hazards that allows the end users to better communicate turbulence as a state of the atmosphere metric and the additional weather threats affecting the flight is described. The method provides an Atmospheric State Index (ASI) that allows all the users to work with a standardized metric that describes the turbulence as the state of the atmosphere and a similar scale for other weather risks to the flight. This system makes the correlation between the forecast and aircraft reports for turbulence easier to interpret for the end users. This approach concentrates on turbulence as a weather hazard with a more objective and easier to use metric. This configuration provides a transition for moving from a system based on turbulence Pilot Reports (PIREPS) to a more objective data driven process in the air traffic environment.

Claims (39)

1. A computer-implemented method for facilitating the execution of a path of air travel, said method comprising the steps of:

receiving, via one or more processors, hazard data indicative of a deterministic intensity of at least two hazards of at least two hazard types, wherein the deterministic intensity of each of the at least two hazards is determined based at least in part on a forecast model;

converting, via the one or more processors, the deterministic intensity of each of the at least two hazards indicated by the hazard data to fit an atmospheric state intensity scale, the atmospheric state intensity scale consisting of and being defined by a plurality of deterministic intensity values that are each common across each of a plurality of hazard types, such that the hazard data is indicative of the deterministic intensity of each of the at least two hazards along said atmospheric state intensity scale, wherein a value of each of said plurality of deterministic intensity values is indicative of the deterministic intensity of each of said at least two hazards; and

generating, via a display device in communication with the one or more processors, a graphical display indicative of: a path of air travel and the deterministic intensity of said at least two hazards along said atmospheric state intensity scale.

2. The method of claim 1 , wherein said at least two hazards types comprise turbulence and icing.

3. The method of claim 1 , wherein said hazard data comprises data dependent at least in part upon aircraft response characteristics.

4. The method of claim 1 , wherein said hazard data comprises data indicative of live reports of observed hazard conditions; and said graphical display is further indicative of the location of the live reports.

5. The method of claim 1 , further comprising the step of:

organizing, via the one or more processors, at least a portion of said hazard data into a plurality of data points corresponding to the at least two hazards, each of said plurality of data points comprising information indicative of at least one of: the hazard type, a hazard location in a three-dimensional space, the deterministic intensity of the hazard, or a hazard probability indicative of a probability associated with the at least two hazards, and a time.

6. The method of claim 1 , further comprising steps for:

establishing at least one travel tolerance parameter (TTP) following said atmospheric state intensity scale for each of said at least two hazard types; and

determining, based at least in part on the hazard data and the at least one TTP, an executable path of air travel that satisfies the at least one TTP.

7. The method of claim 6 , wherein said at least one TTP is established at least partially in light of one of pilot training, employer guidelines, a flight equipment type, or other pilots.

8. The method of claim 6 , wherein said at least one TTP comprises a probability element.

9. The method of claim 6 , further comprising the step of:

generating, via the one or more computer processors, an altered path of air travel based at least in part on the path of air travel, changes in the hazard data, and upon recognition that said path of air travel is incompatible with the at least one TTP.

10. The method of claim 9 , further comprising steps for:

determining an expected completion time of said path of air travel; and

updating the expected completion time of said path of air travel based on the altered path of air travel.

11. The method of claim 1 , wherein said graphical display comprises a color gradation corresponding to one or more deterministic intensity values of the atmospheric state intensity scale.

12. The method of claim 6 , further comprising the step of generating an alert upon a determination that the at least one TTP is not satisfied by the hazard data.

13. A hazard avoidance system for facilitating the execution of a path of air travel, the system comprising:

one or more memory storage areas; and

one or more computer processors configured to:

receive hazard data indicative of a deterministic intensity of at least two hazards of at least two hazard types, wherein the deterministic intensity of each of the at least two hazards is determined based at least in part on a forecast model;

convert the deterministic intensity of each of the at least two hazards indicated by the hazard data to fit an atmospheric state intensity scale, the atmospheric state intensity scale consisting of and being defined by a plurality of deterministic intensity values that are each common across each of a plurality of hazard types, such that the hazard data is indicative of the deterministic intensity of each of the at least two hazards along said atmospheric state intensity scale, wherein a value of each of said plurality of deterministic intensity values is indicative of the deterministic intensity of each of said at least two hazards; and

generate a graphical display indicative of: a path of air travel and the deterministic intensity of said at least two hazards along said atmospheric state intensity scale.

14. The system of claim 13 , wherein the one or more processors are further configured to:

establish at least one travel tolerance parameter (TTP) following said atmospheric state intensity scale for each of said at least two hazard types; and

determine, based at least in part on the hazard data and the at least one TTP, an executable path of air travel that satisfies the at least one TTP.

15. The system of claim 14 , wherein the one or more computer processors are further configured to generate an alert upon a determination that the at least one TTP is not satisfied by the hazard data.

16. A non-transitory computer program product comprising at least one computer-readable storage medium having computer-readable program code portions embodied therein, the computer-readable program code portions comprising at least one executable portion configured for:

receiving hazard data indicative of a deterministic intensity of at least two hazards of at least two hazard types, wherein the deterministic intensity of each of the at least two hazards is determined based at least in part on a forecast model;

converting the deterministic intensity of each of the at least two hazards indicated by the hazard data to fit an atmospheric state intensity scale, the atmospheric state intensity scale consisting of and being defined by a plurality of deterministic intensity values that are each common across each of a plurality of hazard types, such that the hazard data is indicative of the deterministic intensity of each of the at least two hazards along said atmospheric state intensity scale, wherein a value of each of said plurality of deterministic intensity values is indicative of the deterministic intensity of each of said at least two hazards; and

generating a graphical display indicative of: a path of air travel and the deterministic intensity of said at least two hazards along said atmospheric state intensity scale.

17. The non-transitory computer program product of claim 16 , wherein the at least one executable portion is further configured for:

establishing at least one travel tolerance parameter (TTP) following said atmospheric state intensity scale for each of said at least one hazard type; and

determining, based at least in part on the hazard data and the at least one TTP, an executable path of air travel that satisfies the at least one TTP.

18. The non-transitory computer program product of claim 17 , wherein the at least one executable portion is further configured to generate an alert upon a determination that the at least one TTP is not satisfied by the hazard data.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 31, 2021
From: DELTA AIR LINES, INC.
To: BLUE EAGLE FUND, LLC
Reel/Frame 057340/0767 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 22, 2015
From: BLUE EAGLE FUND, LLC
To: DELTA AIR LINES, INC.
Reel/Frame 037353/0009 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 22, 2015
From: WATTS, WILLIAM HENRY
To: BLUE EAGLE FUND, LLC
Reel/Frame 037353/0105 →
Continuity (3)
Continuation 13781573 · Feb 28, 2013
Provisional Application 61604022 · Feb 28, 2012
Related Publication 20160155340A1 · Jun 2, 2016